High fidelity aeroelastic prediction - Texte

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Forschungsstelle

INNOSUISSE

Projektnummer

14323.2 PFIW-IW

Projekttitel

High fidelity aeroelastic prediction

Projekttitel Englisch

High fidelity aeroelastic prediction

Texte zu diesem Projekt

	Deutsch	Französisch	Italienisch	Englisch
Kurzbeschreibung		-	-
Abstract		-	-

Erfasste Texte

Kategorie	Text
Kurzbeschreibung (Deutsch)	High fidelity aeroelastic prediction
Kurzbeschreibung (Englisch)	High fidelity aeroelastic prediction
Abstract (Deutsch)	The project concerns the development of a prediction method based on high-fidelity simulation tools. it is a first, but\|critical, step towards the development of a high-fidelity numerical method able to predict the dynamical behaviour of\|EASA-C23 aircraft (Max Take-Off Mass below 3.5 tons). High-fidelity aerodynamic and structural modelling is essential\|to keep into account the highly non-linear nature of the physics involved.
Abstract (Englisch)	The project concerns the development of a prediction method based on high-fidelity simulation tools. it is a first, but\|critical, step towards the development of a high-fidelity numerical method able to predict the dynamical behaviour of\|EASA-C23 aircraft (Max Take-Off Mass below 3.5 tons). High-fidelity aerodynamic and structural modelling is essential\|to keep into account the highly non-linear nature of the physics involved.